AD/BEECH 35/41 Amdt 1 - Landing Gear Shock Strut Piston

Overview

The Civil Aviation Regulations 1998, as amended, address the safety and operational standards for civil aviation within Australia. One particular legislative instrument, F2006B03839, pertains to the issue of airworthiness directives, specifically focusing on the Beechcraft 35 (Bonanza) series aeroplanes. This legislative instrument was introduced to ensure that these aircraft meet stringent safety standards, particularly concerning the landing gear shock strut piston. The objective is to maintain and enhance the safety of civil aviation by enforcing compliance with specific maintenance and operational requirements. Enacted by the Parliament of Australia, this regulation falls under the broader scope of the Civil Aviation Act 1988, which aims to protect public safety through the regulation of civil aviation. This legislative instrument is part of a series of measures designed to mitigate risks associated with aircraft operation by imposing mandatory actions on specific aircraft models. In this case, AD/BEECH 35/41 Amendment 1 targets all model V35B Beechcraft Bonanza aeroplanes with serial numbers ranging from D9469 to D9536, excluding D9481, D9532, and D9533. The requirement stipulates that corrective action must be taken in accordance with Beechcraft Service Instruction No. 0612-200, with compliance needed within 100 hours of time in service following 31 January 1974, unless the action has already been completed. This directive aims to ensure that the specified aircraft meet the necessary safety standards, thereby enhancing overall aviation safety.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the safety directives governing airworthiness, as detailed in the schedule of airworthiness directives. The regulations are pertinent to the Beechcraft 35 (Bonanza) series aeroplanes, focusing on the landing gear shock strut piston, and cover all model V35B aircraft with serial numbers ranging from D9469 to D9536, excluding specific aircraft with serial numbers D9481, D9532, and D9533. The directive mandates compliance with Beechcraft Service Instruction No. 0612-200 and requires that the specified action be completed within 100 hours of time in service after 31 January 1974, unless the action has already been undertaken. The regulations are applicable across the Commonwealth of Australia and are enforced by the Civil Aviation Safety Authority. The scope and application of these directives are not restricted by additional exclusions, exemptions, or thresholds as specified in the legislation, and any further detail or extension of application is to be found in subordinate instruments.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address airworthiness directives related to certain aircraft models, with a focus on the Beechcraft 35 (Bonanza) Series Aeroplanes. This particular legislative instrument, AD/BEECH 35/41 Amendment 1, pertains to the landing gear shock strut piston of model V35B aeroplanes with specific serial numbers (sections 1-74). The requirement outlined in this directive is for compliance with Beechcraft Service Instruction No. 0612-200, which likely details the necessary modifications or inspections to ensure the airworthiness of the aircraft. The obligations imposed by this legislation are clear and direct. Aircraft operators must ensure that the specified Beechcraft 35 (Bonanza) Series aeroplanes undergo the required action regarding the landing gear shock strut piston within 100 hours of time in service following 31 January 1974. This action must be completed unless it has already been accomplished prior to the effective date of the directive. The directive specifically excludes certain serial numbers (D9481, D9532, and D9533) from the applicability of this requirement. Failure to comply with the airworthiness directive can lead to significant consequences. While the specific penalties for non-compliance are not detailed within the text provided, it is understood that non-compliance with such directives can result in serious civil or criminal penalties under the Civil Aviation Act 1988 and related regulations. These penalties could include fines, enforcement actions, or even the grounding of the aircraft, which can severely impact the operations of the aircraft owner or operator. The seriousness of these potential consequences underscores the importance of adhering to the directive to maintain the safety standards required by the Civil Aviation Safety Authority.